scholarly journals SOUNDING ROCKET MICROGRAVITY EXPERIMENTS ELUCIDATING DIFFUSIVE AND RADIATIVE TRANSPORT EFFECTS ON FLAME SPREAD OVER THERMALLY THICK SOLIDS

2004 ◽  
Vol 176 (4) ◽  
pp. 557-584 ◽  
Author(s):  
S. L. OLSON∗ ◽  
U. HEGDE ◽  
S. BHATTACHARJEE ◽  
J. L. DEERING ◽  
L. TANG ◽  
...  
Author(s):  
Yanjun Li ◽  
Ya-Ting T. Liao ◽  
Paul Ferkul

Abstract A numerical study is pursued to investigate the aerodynamics and thermal interactions between a spreading flame and the surrounding walls as well as their effects on fire behaviors. This is done in support of upcoming microgravity experiments aboard the International Space Station. For the numerical study, a three-dimensional transient Computational Fluid Dynamics combustion model is used to simulate concurrent-flow flame spread over a thin solid sample in a narrow flow duct. The height of the flow duct is the main parameter. The numerical results predict a quenching height for the flow duct below which the flame fails to spread. For duct heights sufficiently larger than the quenching height, the flame reaches a steady spreading state before the sample is fully consumed. The flame spread rate and the pyrolysis length at steady state first increase and then decrease when the flow duct height decreases. The detailed gas and solid profiles show that flow confinement has competing effects on the flame spread process. On one hand, it accelerates flow during thermal expansion from combustion, intensifying the flame. On the other hand, increasing flow confinement reduces the oxygen supply to the flame and increases conductive heat loss to the walls, both of which weaken the flame. These competing effects result in the aforementioned non-monotonic trend of flame spread rate as duct height varies. This work relates to upcoming microgravity experiments, in which flat thin samples will be burned in a low-speed concurrent flow using a small flow duct aboard the International Space Station. Two baffles will be installed parallel to the fuel sample (one on each side of the sample) to create an effective reduction in the height of the flow duct. The concept and setup of the experiments are presented in this work.


2018 ◽  
Vol 30 (4) ◽  
pp. 535-542 ◽  
Author(s):  
Masato Mikami ◽  
Yasuko Yoshida ◽  
Takehiko Seo ◽  
Tetsuya Sakashita ◽  
Masao Kikuchi ◽  
...  

2006 ◽  
Vol 146 (3) ◽  
pp. 391-406 ◽  
Author(s):  
Masato Mikami ◽  
Hiroshi Oyagi ◽  
Naoya Kojima ◽  
Yuichiro Wakashima ◽  
Masao Kikuchi ◽  
...  

2018 ◽  
Vol 9 (1) ◽  
Author(s):  
Shinnosuke Ishizuka ◽  
Yuki Kimura ◽  
Itsuki Sakon ◽  
Hiroshi Kimura ◽  
Tomoya Yamazaki ◽  
...  

2005 ◽  
Vol 141 (3) ◽  
pp. 241-252 ◽  
Author(s):  
M MIKAMI ◽  
H OYAGI ◽  
N KOJIMA ◽  
M KIKUCHI ◽  
Y WAKASHIMA ◽  
...  

2002 ◽  
Vol 29 (2) ◽  
pp. 2603-2610 ◽  
Author(s):  
Hideaki Kobayashi ◽  
Jeong Park ◽  
Takeshi Iwahashi ◽  
Takashi Niioka

1988 ◽  
Vol 102 ◽  
pp. 259-261
Author(s):  
W.A. Brown ◽  
M.E. Bruner ◽  
L.W. Acton
Keyword(s):  

AbstractThe soft x-ray spectra recorded in two sounding rocket flights in 1982 and 1985 are compared with with predicted spectra. The poster presents the processed densitometer trace of the full spectrum together with the new spectrum from the 1985 experiment. This note compares the intensities of the lines with predictions.


2015 ◽  
Vol 46 (7) ◽  
pp. 673-687 ◽  
Author(s):  
Hengze Zhao ◽  
Yongming Zhang ◽  
Yuanming Wang ◽  
Lanming Zhao
Keyword(s):  

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